Dynamic Characteristics of Aircraft Landing Gear-Reference-Cited by-同舟云学术

Dynamic Characteristics of Aircraft Landing Gear

Published:2014-03 Issue: Volume:543-547 Page:118-121
ISSN:1662-7482
Container-title:Applied Mechanics and Materials
language:
Short-container-title:AMM

Author:

Yu Jing Wei¹,Liu Xiao Feng¹,Wang Hai Long¹,Wei Yu Jian¹

Affiliation:

1. Air Force Aviation University

Abstract

Aircraft landing gear can absorb the energy generated and consumed in aircraft landing, taxiing process, thus weakening the vibration of the aircraft, flight safety plays a vital role. This paper established a landing gear dynamics modeling, its mechanical analysis, and through trial and simulation of the dynamic characteristics of the landing gear were studied, with some practical significance.

Publisher

Trans Tech Publications, Ltd.

Link

https://www.scientific.net/AMM.543-547.118.pdf

Reference5 articles.

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3. Sun Shi-hui. Research on the Landing Dynamic Performance for a Certain Type of Aircraft Landing Gear[D]. Jilin University, (2009).

4. W. Krüger. Design and simulation of semi-active landing gears for transportaircraft, Mechanics of Structures and Machines, 2002, 30(4): 493-526.

5. G.L. Ghiringhelli,S. Gualdi, Evaluation of a landing gear semi-active control system for complete aircraft landing, Aerotecnica Missili e Spazio, 2004, 83(1): 21-29.

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